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时间:2011-03-27 00:00来源:蓝天飞行翻译 作者:admin
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 (21) on the Bulk door frame and the floor panel 162KF.

 (6)
 Install the sidewall panels 162BW and 162EW with the related quick-release fasteners.

 (7)
 Close the Bulk cargo-compartment door (Ref. TASK 52-30-00-860-011).


 (8) Remove the access platform(s). R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
 Subtask 52-33-32-865-052
 C. Make sure that this(these) circuit breaker(s) is(are) closed: 46WV.
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-32Page 415 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 Adjustment of Door Frame Fittings
 Figure 402/TASK 52-33-32-991-002

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-32Page 416 1224-224, 228-228, 1May 01/05 1 1 1CES 1 BALANCE MECHANISM - REMOVAL/INSTALLATION


________________________________________
 TASK 52-33-41-000-001
 Removal of the Balance Mechanism
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific adjustment gage
 No specific support device
 No specific access platform 2.10 m (6 ft. 11 in.)
 No specific access platform 2.30 m (7 ft. 7 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump 52-30-00-860-006 Open the Bulk Cargo-Compartment Door 52-30-00-860-008 Close the Bulk Cargo-Compartment Door 52-30-00-860-010 Open the Deactivated Bulk Cargo-Compartment Door 52-33-13-000-001 Removal of the Lining and Insulation of the Bulk
 Cargo-Compartment Door 52-33-41-991-001 Fig. 401 52-33-41-991-002 Fig. 402 52-33-41-991-003 Fig. 403
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-41Page 401 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 3. Job Set-up
__________
 Subtask 52-33-41-010-050

 A. Get Access
 (1)
 Open the AFT cargo-compartment door (Ref. TASK 52-30-00-860-001) to get access to the inner side of the closed Bulk cargo-compartment door (referred to as Bulk cargo door).

 (2)
 Put the access platform 2.10 m (6 ft. 11 in.) in position at the AFT cargo-compartment door.

 (3)
 Remove the divider net at FR59 to get access to the Bulk cargo compartment.

 (4)
 Remove the door net from the opening of the Bulk cargo compartment to get access to the closed Bulk cargo door.

 (5)
 Remove the lining from the Bulk door and the insulation from the work area (Ref. TASK 52-33-13-000-001).

 (6)
 Put the access platform 2.30 m (7 ft. 7 in.) in position at the Bulk door.


 4. Procedure
_________ (Ref. Fig. 401/TASK 52-33-41-991-001, 402/TASK 52-33-41-991-002, 403/TASK 52-33-41-991-003) R **ON A/C 001-049, 051-099, 101-105,
 Subtask 52-33-41-020-050
 A. Removal of the Connection Road
 (1) Release the tension of the balance mechanism as follows:
 (a) Install the adjustment gage between the forward lever (15) and the stop fitting of the beam 2.
 NOTE : The permitted tolerance of the adjustment gage thickness
____ is between 17.7 mm (0.6968 in.) and 18.3 mm (0.7204 in.).
 (b) Fully open the Bulk door (Ref. TASK 52-30-00-860-006).
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-41Page 402 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 Connection Rod and Pre-Load Unit
 Figure 401/TASK 52-33-41-991-001

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-41Page 403 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 Torsion Spring
 Figure 402/TASK 52-33-41-991-002

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-41Page 404 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 Adjustment Gage of Balance Mechanism
 Figure 403/TASK 52-33-41-991-003

R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-41Page 405 1224-224, 228-228, 1May 01/05 1 1 1CES 1


 (2)
 Disconnect the connection rod (11) from the fuselage fitting (4) as follows:

 (a)
 Remove and discard the cotter pin (1) from the castle nut (2).

 (b)
 Remove the castle nut (2), the washers (3), and the bolt (5).
 
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